View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56040U 26145.48489036 +.00000000 +00000-0 +62728-5 0 00008
2 56040 43.0036 317.3248 0001694 269.9475 90.1183 15.27573044 03
| Epoch (UTC): | 25 May 2026 11:38:14 |
| Eccentricity: | 0.0001694 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.3248° |
| argument of perigee: | 269.9475° |
| revolutions per day: | 15.27573044 |
| mean anomaly at epoch: | 90.1183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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